US5760357A - Thrust detecting device of a linear actuator - Google Patents
Thrust detecting device of a linear actuator Download PDFInfo
- Publication number
- US5760357A US5760357A US08/569,693 US56969395A US5760357A US 5760357 A US5760357 A US 5760357A US 56969395 A US56969395 A US 56969395A US 5760357 A US5760357 A US 5760357A
- Authority
- US
- United States
- Prior art keywords
- striker
- screw shaft
- plate
- pinion
- drive screw
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
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Classifications
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H19/00—Switches operated by an operating part which is rotatable about a longitudinal axis thereof and which is acted upon directly by a solid body external to the switch, e.g. by a hand
- H01H19/54—Switches operated by an operating part which is rotatable about a longitudinal axis thereof and which is acted upon directly by a solid body external to the switch, e.g. by a hand the operating part having at least five or an unspecified number of operative positions
- H01H19/60—Angularly-movable actuating part carrying no contacts
- H01H19/62—Contacts actuated by radial cams
- H01H19/623—Adjustable cams
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H35/00—Switches operated by change of a physical condition
- H01H35/006—Switches operated by mechanical overload condition, e.g. transmitted force or torque becoming too high
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16H—GEARING
- F16H25/00—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms
- F16H25/18—Gearings comprising primarily only cams, cam-followers and screw-and-nut mechanisms for conveying or interconverting oscillating or reciprocating motions
- F16H25/20—Screw mechanisms
-
- H—ELECTRICITY
- H01—ELECTRIC ELEMENTS
- H01H—ELECTRIC SWITCHES; RELAYS; SELECTORS; EMERGENCY PROTECTIVE DEVICES
- H01H3/00—Mechanisms for operating contacts
- H01H3/32—Driving mechanisms, i.e. for transmitting driving force to the contacts
- H01H3/40—Driving mechanisms, i.e. for transmitting driving force to the contacts using friction, toothed, or screw-and-nut gearing
Definitions
- the present invention relates to a thrust detecting device for detecting a change or variation in the thrust load acting on an actuating rod of an electrically operated linear actuator to control the thrust or axial displacement of the actuating rod.
- a conventional thrust detecting means or device associated with the actuating rod of a linear actuator is constructed such that an axial leftward displacement of a rotating drive screw shaft 31 caused due to a change in the thrust load, such as an overload, acting on the screw shaft 31 continuously rotating to advance the actuating rod 30 causes an axial leftward movement of a striker 34 attached to a thrust flange 33 of a thrust load change absorbing spring 32, and the axial leftward displacement thus caused is detected when a limit switch LA is activated by the striker 34.
- LA and LB are overload detecting limit switches, respectively, for a forward or pushing stroke and a backward or pulling stroke.
- the moving distance of the striker may be enlarged if the absorbing spring is replaced with another spring having a smaller spring constant and a larger length so as to allow the shaft to be axially displaced over a longer distance than before.
- the present invention provides a solution to the foregoing problem of the prior art in that an axial displacement of a rotating drive screw shaft caused due to a change in the thrust load on the screw shaft while being rotated to drive the actuating rod of a linear actuator is not automatically used as a linear movement of a striker but instead is enlarged by being converted into an angular displacement of the striker.
- the present invention further provides a thrust detecting device of the linear actuator, which comprises: a thrust load change absorbing spring fitted around the rotating drive screw shaft; a thrust flange rotatably mounted on the actuating drive screw shaft for thrusting the absorbing spring and having a tubular portion; a plurality of annular threaded teeth formed on an outer peripheral surface of the tubular portion; a pinion meshing with the annular threaded teeth and having a vertical shaft projecting into a limit switch box mounted on an upper portion of a housing of the linear actuator; a circular scale plate secured to a front end of the projecting vertical shaft; a large-diameter striker plate having formed therewith a radially projecting pointer and a radially projecting limit-switch actuating striker and attached to a center of the circular scale plate such that the striker plate is rotatable over the circular scale plate about the center thereof.
- the axial displacement of the screw shaft causes the pinion to angularly move or turn via meshing engagement between the pinion and the annular threaded teeth formed on the outer peripheral surface of the tubular portion of the thrust flange acting on the thrust load change absorbing spring rotatably fitted around the screw shaft.
- the circular scale plate is turned because it is secured to the front end of the vertical shaft of the pinion which projects into the limit switch box.
- the large-diameter striker plate which is rotatably attached to the circular scale plate rotates together with the circular scale plate.
- a working distance between the striker and the corresponding limit switch fixed at a given position is automatically set to a value equal to the reading of the scale mark.
- the axial linear displacement of the screw shaft caused due to a change in the thrust load is enlarged by being converted into an angular displacement of the circular scale plate via meshing engagement between the annular threaded teeth and the pinion.
- FIG. 1 is a cross-sectional view, in front elevation, of a linear actuator according to the present invention
- FIG. 2 is an enlarged cross-sectional view of an essential part of FIG. 1;
- FIG. 3 is a cross-sectional view taken along the line 3--3 of FIG. 2;
- FIG. 4 is a cross-sectional view taken along the line 4--4 of FIG. 3;
- FIG. 5 is an enlarged view of an essential part of FIG. 4.
- FIG. 6 is a cross-sectional view, in front elevation, of a conventional linear actuator device.
- FIG. 1 is a cross-sectional view, with parts in front elevation, of a linear actuator according to the present invention.
- the linear actuator of FIG. 1 is similar in structure to the conventional linear actuator of FIG. 6 to the extent that it has a structure in which a motor M rotates a rotating drive screw shaft (hereinafter referred to as "screw shaft") 1 whereupon a nut 2 threaded with the screw shaft 1 and an actuating rod 3 joined with the nut 3 are caused to move together back and forth along the screw shaft 1 to thereby reciprocate a movable part or object (not shown) connected to a front end 3A of the actuating rod 3.
- screw shaft rotating drive screw shaft
- a thrust detecting device includes a spring 4 loosely fitted around the screw shaft 1 for absorbing a change or variation of the thrust load acting on the screw shaft 1 via the actuating rod 3, and a flange 5 rotatably mounted on the screw shaft 1 for forcing or thrusting the spring 4.
- the flange 5 has a tubular portion 5A having a plurality of annular threaded teeth 5B formed on its outer peripheral surface.
- a pinion 6 is held in mesh with the annular threaded teeth 5B.
- the pinion 6 has a vertical shaft 6A rotatably supported or journaled by a sleeve 7 firmly fitted in a through-hole in a housing H, as shown in FIG. 3.
- the vertical shaft 6A has a front end portion projecting into a limit switch box 8 attached to an upper portion of the housing H.
- the striker plates 10A and 10B each have a radially outwardly projecting pointer 11A, 11B, a radially outwardly projecting striker 12A, 12B, and an arcuate oblong hole (not numbered) through which an adjustment screw 13A, 13B is threaded into the circular scale plate 9 to secure the corresponding striker plate 10A, 10B to the circular scale plate 9.
- each striker plate 10A, 10B may be turned about the center of the vertical shaft 6A until its pointer 11A, 11B is in alignment with a desired scale mark on the circular scale plate 9.
- the adjustment screw 13A, 13B is tightly fastened to set an angular distance through which each of the strikers 12A, 12B must travel to enable the striker 12A or 12B to activate a corresponding limit switch LA, LB disposed near each respective striker 12A, 12B.
- the opposite end extremities of the allowable axial displacement of the screw shaft 1, at which rotation of the screw shaft 1 is to be stopped, are thus set by the pointers 11A, 11B aligned with the corresponding scale marks on the circular scale plate 9. Accordingly, when the screw shaft 1 is being axially displaced in one direction, such as for example the advancing direction, arrives at a corresponding one of the end extremities of the preset allowable axial displacement of the screw shaft 1, the striker 12A or 12B activates the limit switch LA or LB to stop rotation of the screw shaft 1, thereby stopping advancing movement of the actuating rod 3.
- each striker plate 10A, 10B is secured to a circular scale plate 9 with its pointer 11A, 11B aligned with a desired scale mark on the circular scale plate 9 to thereby set the limit of an allowable change or variation in the thrust load in one direction. Accordingly, when the thrust load change limit is reached, this moment can be detected in terms of activation of the limit switch LA, LB.
- the axial linear displacement of the screw shaft 1 caused due to a thrust load change or variation is enlarged by being converted into an angular displacement of the vertical shaft 6A via meshing engagement between the annular threaded teeth SB and the pinion 6.
Landscapes
- Force Measurement Appropriate To Specific Purposes (AREA)
- Rotary Switch, Piano Key Switch, And Lever Switch (AREA)
- Transmission Devices (AREA)
Abstract
A device for detecting a change in the thrust load acting on the actuating rod of a linear actuator. The thrust detecting device includes a pinion which converts and enlarges an axial linear displacement of a rotating drive screw shaft caused by a change in the load on an actuating rod driven by the screw shaft into an angular displacement of a vertical shaft of the pinion. A circular scale plate is attached to the vertical shaft of the pinion and serves to indicate a preset value for the load change to be detected. A pair of striker plates each having a pointer effective to select a preset value on the circular scale plate and a striker effective to activate a corresponding limit switch are attached to the circular scale plate.
Description
1. Field of the Invention
The present invention relates to a thrust detecting device for detecting a change or variation in the thrust load acting on an actuating rod of an electrically operated linear actuator to control the thrust or axial displacement of the actuating rod.
2. Description of the Related Art
A conventional thrust detecting means or device associated with the actuating rod of a linear actuator, as shown here in FIG. 6, for example, is constructed such that an axial leftward displacement of a rotating drive screw shaft 31 caused due to a change in the thrust load, such as an overload, acting on the screw shaft 31 continuously rotating to advance the actuating rod 30 causes an axial leftward movement of a striker 34 attached to a thrust flange 33 of a thrust load change absorbing spring 32, and the axial leftward displacement thus caused is detected when a limit switch LA is activated by the striker 34.
Designated by LA and LB are overload detecting limit switches, respectively, for a forward or pushing stroke and a backward or pulling stroke.
In the conventional thrust detecting device thus constructed, since movement of the striker relies on an axial linear displacement of the screw shaft caused due to a change in the thrust load acting on the screw shaft, only a small moving distance or travel of the striker can be obtained. With only a small moving distance available, it is difficult to provide an accurate adjustment of the position where each of the limit switches is activated by the striker. To facilitate the adjustment, the moving distance of the striker may be enlarged if the absorbing spring is replaced with another spring having a smaller spring constant and a larger length so as to allow the shaft to be axially displaced over a longer distance than before.
However, such an enlargement of the axial movement of the striker will cause a problem in that an oblong hole 35, elongated to accommodate the enlarged angular movement of the striker, is likely to accept the entry of foreign matter, leading to a loss of the detecting function of the limit switches.
The present invention provides a solution to the foregoing problem of the prior art in that an axial displacement of a rotating drive screw shaft caused due to a change in the thrust load on the screw shaft while being rotated to drive the actuating rod of a linear actuator is not automatically used as a linear movement of a striker but instead is enlarged by being converted into an angular displacement of the striker. The present invention further provides a thrust detecting device of the linear actuator, which comprises: a thrust load change absorbing spring fitted around the rotating drive screw shaft; a thrust flange rotatably mounted on the actuating drive screw shaft for thrusting the absorbing spring and having a tubular portion; a plurality of annular threaded teeth formed on an outer peripheral surface of the tubular portion; a pinion meshing with the annular threaded teeth and having a vertical shaft projecting into a limit switch box mounted on an upper portion of a housing of the linear actuator; a circular scale plate secured to a front end of the projecting vertical shaft; a large-diameter striker plate having formed therewith a radially projecting pointer and a radially projecting limit-switch actuating striker and attached to a center of the circular scale plate such that the striker plate is rotatable over the circular scale plate about the center thereof.
In the present invention, when the rotating drive screw shaft held in threaded engagement with the actuating rod is axially displaced due to a change in the thrust load acting on the actuating rod being driven, the axial displacement of the screw shaft causes the pinion to angularly move or turn via meshing engagement between the pinion and the annular threaded teeth formed on the outer peripheral surface of the tubular portion of the thrust flange acting on the thrust load change absorbing spring rotatably fitted around the screw shaft. As the pinion turns, the circular scale plate is turned because it is secured to the front end of the vertical shaft of the pinion which projects into the limit switch box. The large-diameter striker plate which is rotatably attached to the circular scale plate rotates together with the circular scale plate.
When the striker plate is secured to the circular scale plate with the pointer aligned with a desired scale mark on the circular scale plate, a working distance between the striker and the corresponding limit switch fixed at a given position is automatically set to a value equal to the reading of the scale mark. The axial linear displacement of the screw shaft caused due to a change in the thrust load is enlarged by being converted into an angular displacement of the circular scale plate via meshing engagement between the annular threaded teeth and the pinion. When the striker has traveled through the preset working distance, it activates the limit switch to stop operation of a drive motor of the screw shaft, thereby stopping axial movement of the actuating rod.
The invention will be described in further detail with reference to the drawings.
FIG. 1 is a cross-sectional view, in front elevation, of a linear actuator according to the present invention;
FIG. 2 is an enlarged cross-sectional view of an essential part of FIG. 1;
FIG. 3 is a cross-sectional view taken along the line 3--3 of FIG. 2;
FIG. 4 is a cross-sectional view taken along the line 4--4 of FIG. 3;
FIG. 5 is an enlarged view of an essential part of FIG. 4; and
FIG. 6 is a cross-sectional view, in front elevation, of a conventional linear actuator device.
FIG. 1 is a cross-sectional view, with parts in front elevation, of a linear actuator according to the present invention. The linear actuator of FIG. 1 is similar in structure to the conventional linear actuator of FIG. 6 to the extent that it has a structure in which a motor M rotates a rotating drive screw shaft (hereinafter referred to as "screw shaft") 1 whereupon a nut 2 threaded with the screw shaft 1 and an actuating rod 3 joined with the nut 3 are caused to move together back and forth along the screw shaft 1 to thereby reciprocate a movable part or object (not shown) connected to a front end 3A of the actuating rod 3. Due to the structural similarity with the conventional linear actuator of FIG. 6, a further detailed description of this structure will be omitted.
As shown in enlarged scale in FIG. 2, a thrust detecting device according to the present invention includes a spring 4 loosely fitted around the screw shaft 1 for absorbing a change or variation of the thrust load acting on the screw shaft 1 via the actuating rod 3, and a flange 5 rotatably mounted on the screw shaft 1 for forcing or thrusting the spring 4. The flange 5 has a tubular portion 5A having a plurality of annular threaded teeth 5B formed on its outer peripheral surface. A pinion 6 is held in mesh with the annular threaded teeth 5B.
The pinion 6 has a vertical shaft 6A rotatably supported or journaled by a sleeve 7 firmly fitted in a through-hole in a housing H, as shown in FIG. 3. The vertical shaft 6A has a front end portion projecting into a limit switch box 8 attached to an upper portion of the housing H.
A circular scale plate 9 having a large diameter, such as shown on enlarged scale in FIGS. 4 and 5, is fixedly secured to the projecting front end portion of the vertical shaft 6A. similarly, a pair of striker plates 10A and 10B are laid over the circular scale plate 9 and attached to the projecting front end of the vertical shaft 6A such that each striker plate 10A, 10B is rotatable about a center of the vertical shaft 6A. The striker plates 10A and 10B each have a radially outwardly projecting pointer 11A, 11B, a radially outwardly projecting striker 12A, 12B, and an arcuate oblong hole (not numbered) through which an adjustment screw 13A, 13B is threaded into the circular scale plate 9 to secure the corresponding striker plate 10A, 10B to the circular scale plate 9. When the adjustment screw 13A, 13B is loosened, each striker plate 10A, 10B may be turned about the center of the vertical shaft 6A until its pointer 11A, 11B is in alignment with a desired scale mark on the circular scale plate 9. Then, the adjustment screw 13A, 13B is tightly fastened to set an angular distance through which each of the strikers 12A, 12B must travel to enable the striker 12A or 12B to activate a corresponding limit switch LA, LB disposed near each respective striker 12A, 12B. With this setting of the striker plates 10A, 10B, opposite end extremities or limits of an allowable axial displacement of the screw shaft 1 can be set.
The opposite end extremities of the allowable axial displacement of the screw shaft 1, at which rotation of the screw shaft 1 is to be stopped, are thus set by the pointers 11A, 11B aligned with the corresponding scale marks on the circular scale plate 9. Accordingly, when the screw shaft 1 is being axially displaced in one direction, such as for example the advancing direction, arrives at a corresponding one of the end extremities of the preset allowable axial displacement of the screw shaft 1, the striker 12A or 12B activates the limit switch LA or LB to stop rotation of the screw shaft 1, thereby stopping advancing movement of the actuating rod 3.
According to the present invention, each striker plate 10A, 10B is secured to a circular scale plate 9 with its pointer 11A, 11B aligned with a desired scale mark on the circular scale plate 9 to thereby set the limit of an allowable change or variation in the thrust load in one direction. Accordingly, when the thrust load change limit is reached, this moment can be detected in terms of activation of the limit switch LA, LB. The axial linear displacement of the screw shaft 1 caused due to a thrust load change or variation is enlarged by being converted into an angular displacement of the vertical shaft 6A via meshing engagement between the annular threaded teeth SB and the pinion 6. By properly selecting the ratio of the radius r1 (FIG. 3) of the vertical shaft 6A to the radius r2 (FIG. 3) of rotation of the strikers 12A, 12B of the respective striker plates 10A, 10B, a further enlargement of the angular displacement of the vertical shaft 6A can be obtained in the form of angular movement of the circular scale plate 9 and the striker plates 10A, 10B. With this enlargement of the angular displacement, the circular scale plate 9 is able to have a scale with a larger inter-graduation space or pitch which insures setting of the pointers 11A, 11B with an improved degree of accuracy and the resulting accurate adjustment of the angular position of the striker plates 10A, 10B. Thus, detection of a change in the thrust load can be achieved with high accuracy.
Claims (5)
1. A thrust detecting device for a linear actuator having an actuating rod threaded with a rotating drive screw shaft and movable back and forth along the rotating drive screw shaft, comprising:
a thrust load change absorbing spring fitted around the rotating drive screw shaft;
a thrust flange rotatably mounted on the rotating drive screw shaft for thrusting said absorbing spring and having a tubular portion, said thrust flange being movable back and forth along the rotating drive screw shaft;
a plurality of annular threaded teeth formed on an outer peripheral surface of said tubular portion of said thrust flange;
a pinion meshing with said annular threaded teeth, thereby converting the axial movement of the rotating drive screw shaft to rotation of said pinion;
a pinion shaft rotatably driven by said pinion and having an end distant from said annular threaded teeth;
a support plate secured to said distant end of said pinion shaft and rotatable therewith;
at least one striker plate having a radially projecting limit-switch actuating striker attached to said support plate such that the striker plate is rotatable over said support plate about said pinion shaft, and
at least one limit switch fixedly mounted for engagement by said actuating striker,
wherein said striker plate can be selectively positioned on said support plate to provide a predetermined arcuate distance through which said actuating striker must travel before actuating said at least one limit switch.
2. The thrust detecting device as recited in claim 1,
wherein said support plate is a circular plate having a scale provided thereon,
wherein said striker plate is formed with a radially projecting pointer, and
wherein said striker plate is rotatable over said circular plate to provide said predetermined arcuate distance by selectively positioning said radially projecting pointer relative to said scale.
3. The thrust detecting device as recited in claim 1,
wherein said support plate is a circular plate having a scale provided thereon,
wherein there are two of said at least one striker plate attached to said circular plate for independent rotatable movement over said circular plate,
wherein each of said striker plates being formed with said limit-switch actuating striker and a radially projecting pointer, and
wherein there are two of said at least one limit switch each fixedly mounted for engagement by said actuating striker of a respective one of said striker plates.
4. The thrust detecting device as recited in claim 1,
wherein said rotating drive screw shaft and said actuating rod are provided internally of a linear actuator housing,
wherein a limit switch housing is provided on said linear actuator housing,
wherein said pinion meshes with said annular threaded teeth internally of said linear actuator housing, and
wherein said pinion shaft projects into said limit switch housing.
5. A thrust detecting device for a linear actuator having an actuating rod threaded with a rotating drive screw shaft and movable back and forth along the rotating drive screw shaft, comprising:
a thrust load change absorbing spring fitted around the rotating drive screw shaft;
a thrust flange rotatably mounted on the rotating drive screw shaft for thrusting said absorbing spring and having a tubular portion;
a plurality of annular threaded teeth formed on an outer peripheral surface of said tubular portion of said thrust flange;
a pinion meshing with said annular threaded teeth and having a pinion shaft projecting into a limit switch box mounted on an upper portion of a housing of the linear actuator;
a circular scale plate secured to a front end of said projecting shaft;
at least one striker plate having a diameter larger than a diameter of said projecting shaft and formed with a radially projecting pointer and a radially projecting limit-switch actuating striker attached to a center of said circular scale plate such that the striker plate is rotatable over the circular scale plate about the center thereof; and
a limit switch fixedly mounted for engagement by said actuating striker after said actuating striker is moved through a predetermined arcuate distance by said pinion.
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6-331009 | 1994-12-09 | ||
| JP6331009A JP2736024B2 (en) | 1994-12-09 | 1994-12-09 | Thrust detection device for linear actuator |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US5760357A true US5760357A (en) | 1998-06-02 |
Family
ID=18238807
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US08/569,693 Expired - Fee Related US5760357A (en) | 1994-12-09 | 1995-12-08 | Thrust detecting device of a linear actuator |
Country Status (2)
| Country | Link |
|---|---|
| US (1) | US5760357A (en) |
| JP (1) | JP2736024B2 (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020178848A1 (en) * | 2001-04-25 | 2002-12-05 | Tornos Sa | Shock-absorbing screw module |
| US20080289919A1 (en) * | 2007-05-21 | 2008-11-27 | Bing-Hong Yang | Limit Switch Device for an Actuator |
| US20100044204A1 (en) * | 2006-10-17 | 2010-02-25 | Idem Safety Switches Limited | Safety Switch |
| US20120306419A1 (en) * | 2011-06-02 | 2012-12-06 | Ricoh Company, Ltd. | Motor speed controller and control method |
| US20190135447A1 (en) * | 2017-11-07 | 2019-05-09 | Hamilton Sundstrand Corporation | Electro-mechanical actuator system for opening and closing of aircraft engine cowl doors |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5519965B2 (en) * | 2009-07-03 | 2014-06-11 | 東日本旅客鉄道株式会社 | Tension display type turnbuckle for overhead wire |
| CN113720512B (en) * | 2021-09-01 | 2024-05-14 | 重庆广达自动化设备有限公司 | Thrust detection device of electric actuating mechanism |
Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4307799A (en) * | 1979-12-05 | 1981-12-29 | Andco Actuator Products, Inc. | Linear actuator |
| US4428249A (en) * | 1981-12-04 | 1984-01-31 | Pako Corporation | Gear torque sensor apparatus |
| US4679451A (en) * | 1985-07-02 | 1987-07-14 | Tsubakimoto Chain Co. | Case for driving section of linear actuator |
| US4712441A (en) * | 1985-05-13 | 1987-12-15 | Brunswick Valve & Control, Inc. | Position controlled linear actuator |
| US4727762A (en) * | 1986-01-07 | 1988-03-01 | Tsubakimoto Chain Co. | Driving force support for linear actuator |
| US4763219A (en) * | 1986-11-14 | 1988-08-09 | Tsubakimoto Chain Co. | Overload protection for DC motor-driven linear actuator |
| US4910419A (en) * | 1988-05-16 | 1990-03-20 | Tsubakimoto Chain Co. | Overload detection mechanism for motor-driven linear actuator |
| JPH0462946A (en) * | 1990-07-02 | 1992-02-27 | Fujitsu Ltd | Mounting method of ic chip on liquid-crystal display panel |
| US5564677A (en) * | 1995-02-14 | 1996-10-15 | General Electric Company | Linear actuator with force switch for detecting axial load |
| US5586646A (en) * | 1992-06-16 | 1996-12-24 | Bridgeman; Mark | Vehicle locking systems |
-
1994
- 1994-12-09 JP JP6331009A patent/JP2736024B2/en not_active Expired - Lifetime
-
1995
- 1995-12-08 US US08/569,693 patent/US5760357A/en not_active Expired - Fee Related
Patent Citations (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4307799A (en) * | 1979-12-05 | 1981-12-29 | Andco Actuator Products, Inc. | Linear actuator |
| US4428249A (en) * | 1981-12-04 | 1984-01-31 | Pako Corporation | Gear torque sensor apparatus |
| US4712441A (en) * | 1985-05-13 | 1987-12-15 | Brunswick Valve & Control, Inc. | Position controlled linear actuator |
| US4679451A (en) * | 1985-07-02 | 1987-07-14 | Tsubakimoto Chain Co. | Case for driving section of linear actuator |
| US4727762A (en) * | 1986-01-07 | 1988-03-01 | Tsubakimoto Chain Co. | Driving force support for linear actuator |
| US4763219A (en) * | 1986-11-14 | 1988-08-09 | Tsubakimoto Chain Co. | Overload protection for DC motor-driven linear actuator |
| US4910419A (en) * | 1988-05-16 | 1990-03-20 | Tsubakimoto Chain Co. | Overload detection mechanism for motor-driven linear actuator |
| JPH0462946A (en) * | 1990-07-02 | 1992-02-27 | Fujitsu Ltd | Mounting method of ic chip on liquid-crystal display panel |
| US5586646A (en) * | 1992-06-16 | 1996-12-24 | Bridgeman; Mark | Vehicle locking systems |
| US5564677A (en) * | 1995-02-14 | 1996-10-15 | General Electric Company | Linear actuator with force switch for detecting axial load |
Cited By (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020178848A1 (en) * | 2001-04-25 | 2002-12-05 | Tornos Sa | Shock-absorbing screw module |
| US6776061B2 (en) * | 2001-04-25 | 2004-08-17 | Tornos Sa | Shock-absorbing screw module |
| US20100044204A1 (en) * | 2006-10-17 | 2010-02-25 | Idem Safety Switches Limited | Safety Switch |
| US8089012B2 (en) * | 2006-10-17 | 2012-01-03 | Idem Safety Switches Limited | Safety switch |
| US20080289919A1 (en) * | 2007-05-21 | 2008-11-27 | Bing-Hong Yang | Limit Switch Device for an Actuator |
| US20120306419A1 (en) * | 2011-06-02 | 2012-12-06 | Ricoh Company, Ltd. | Motor speed controller and control method |
| US9024568B2 (en) * | 2011-06-02 | 2015-05-05 | Ricoh Company, Ltd. | Motor speed controller and control method |
| US20190135447A1 (en) * | 2017-11-07 | 2019-05-09 | Hamilton Sundstrand Corporation | Electro-mechanical actuator system for opening and closing of aircraft engine cowl doors |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH08159895A (en) | 1996-06-21 |
| JP2736024B2 (en) | 1998-04-02 |
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